CZ-6A DEB, 61469

Orbit data source: Space-Track

CZ-6A DEB, 61469 is space debris in LEO originally from a launch on Tue, 06 Aug 2024 UTC launched from the Taiyaun Space Center, China (TSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

CZ-6A DEB will be above the set Earth location in 2 hours

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/61469?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/61469?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

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ISO8601 Format

Identifier

61469, 2024-140AAB

Orbit

LEO

Last TLE update

7 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2024-08-06 (9 months ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 7 hours ago

0 CZ-6A DEB
1 61469U 24140AAB 25122.78868555  .00013104  00000-0  18896-2 0  9994
2 61469  90.0456 353.9408 0141021 164.2506 196.3169 14.69572728 37216

Epoch: 2025-05-02T18:55Z

Definitive object data (Epoch: 2025-05-02T18:55:42.431Z)

Latitude

0.00005°

Longitude

-150.92626°

Altitude

760.977 km

Speed

7.423 km/s

True Right ascension

23h 35m 45s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

61.91679°

Longitude

29.16039°

Altitude

602.268 km

Speed

7.602 km/s

Apparent Right ascension

19h 13m 39s

Apparent Declination

39° 24' 39"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

09:44:42

Azimuth

28.297° NE

Elevation

-3.502°

Doppler factor

Orbital elements

Apogee altitude

758.552 km

Perigee altitude

560.066 km

Semi-major axis

7,037.446 km

Eccentricity

0.0141021

Inclination

90.0456°

RAAN

353.9408°

Arg. of periapsis

164.2506°

True anomaly

195.87045°

Mean anomaly

196.3169°

Eccentric anomaly

196.09293°

Mean motion

3.67638 °/min

BSTAR

0.0018896

Orbital period

97.92 mins

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

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Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

QIANFAN-1, 60379

CZ-6A DEB, 60625

CZ-6A DEB, 61468

CZ-6A DEB, 61470 (Decayed)

CZ-6A DEB Visibility forecast

Observer location: undefined°, undefined°

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
7 mins	2025-05-03 03:40:15.620Z	6.319° NNE	2025-05-03 03:44:15.620Z	108.307° ESE	43.767°	2025-05-03 03:47:15.620Z	175.831° S
4 mins	2025-05-03 14:42:15.620Z	102.486° ESE	2025-05-03 14:44:15.620Z	70.804° E	18.422°	2025-05-03 14:46:15.620Z	41.816° NE
7 mins	2025-05-03 16:18:15.620Z	209.738° SW	2025-05-03 16:21:15.620Z	265.279° W	33.154°	2025-05-03 16:25:15.620Z	338.738° N

Authenticating...

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Check out CZ-6A DEB, 61469 on other resources

View CZ-6A DEB, 61469 on Heavens-Above

View CZ-6A DEB, 61469 on Keep Track

View CZ-6A DEB, 61469 on Celestrak

View CZ-6A DEB, 61469 on Gunter's Space Page

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